US7244103B2 - Windmill rotor comprising multiple separate wind channels - Google Patents

Windmill rotor comprising multiple separate wind channels Download PDF

Info

Publication number
US7244103B2
US7244103B2 US10/535,984 US53598405A US7244103B2 US 7244103 B2 US7244103 B2 US 7244103B2 US 53598405 A US53598405 A US 53598405A US 7244103 B2 US7244103 B2 US 7244103B2
Authority
US
United States
Prior art keywords
wind
tubular
round
trapezoids
cylinders
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
US10/535,984
Other versions
US20060182632A1 (en
Inventor
Felix Sanchez Sanchez
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of US20060182632A1 publication Critical patent/US20060182632A1/en
Application granted granted Critical
Publication of US7244103B2 publication Critical patent/US7244103B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H1/00Propulsive elements directly acting on water
    • B63H1/02Propulsive elements directly acting on water of rotary type
    • B63H1/12Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
    • B63H1/14Propellers
    • B63H1/16Propellers having a shrouding ring attached to blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D1/00Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/06Rotors
    • F03D1/0608Rotors characterised by their aerodynamic shape
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/33Shrouds which are part of or which are rotating with the rotor
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

Definitions

  • round honeycomb rotor with bent tubular trapezoids is ideal for wind generators and most propellers. Its purpose is to improve wind generators and propellers performance, which is achieved by a total closure of all the perimeters through the concentric tubular cylinders where the bent pieces, which are mounted upon the tubular cylinders lean on. Everything is assembled in a round honeycomb shape formed by modules of round bent tubular trapezoids, which by receiving all of the wind force multiply over two the number of trapezoids, which at the same time multiply wind contact surfaces over twenty times. Wind generator rotors make the most of the wind force thanks to the multiplication of trapezoids as well as the multiplication of their contact surfaces with the wind. The same applies to most propeller rotors, the multiplication of the number of trapezoids added to the multiplication of their contact surfaces lead to the multiplication and optimum use of the driving centrifugal forces involved.
  • wind generator rotors The technique used in wind generator rotors has varied applications and counts with different dimensions. It generally consists of a pitch with usually three blades fitted in; some models have directional blades easily adaptable to the wind direction.
  • wind generators and most propellers have their outer perimeters widely open being most of the driving centrifugal forces wasted through the propellers.
  • Round honeycomb rotors with round bent tubular trapezoids are ideal for wind generators and most propellers. They consist of several concentric tubular cylinders with bent pieces fitted in between making round tubular trapezoids whose main purpose is to maximise the wind force performance. On the one hand this maximisation in wind generators and propellers is possible by substituting the conventional blades with bent tubular trapezoids, which have the capacity to multiply wind contact surfaces over twenty times. On top of that propellers also maximise most of the propelled centrifugal forces coming from the engine revolutions and going to the blades. On the other hand these trapezoids are fitted into concentric tubular cylinders therefore closing all the trapezoids perimeters giving the rotor a round honeycomb shape.
  • the tubular cylinder with largest diameter has fitted in an open funnel with a conical opening facing outwards in order to increase the wind entry surface to the rotor.
  • Bent tubular trapezoids in conventional wind generators have a soft entrance, which goes diminishing towards the exit creating a small pressure. This is natural in this kind of wind rotors as they have wind entrance and exit areas orientated in the same direction. Nevertheless in this present patent invention, the progressive curving of the bent tubular trapezoids will divert the course of the wind to another direction, which will automatically reduce the wind force as it exits like it happens in wind turbines. Propellers in general will have similar characteristics to wind rotors adding the effect of centrifugal forces.
  • round tubular trapezoids are assembled in several concentric tubular cylinders, which have bent pieces inserted in between each one of them giving the whole structure the shape of a round honeycomb with round bent tubular trapezoids inside.
  • Bent tubular trapezoids in wind generators and propellers could be of any of the well-known geometrical shapes such as round, tubular, oval or polygons with as many regular or irregular sides as needed. Inside the trapezoids similar shapes could be adopted or even other ones such as oblique trapezoids or any rough shapes whose only function would be to minimise the wind force.
  • the tubular cylinder with larger diameter in most propellers rotor has fitted in a conical funnel opening inwards that reduces the wind exit surface therefore minimising the wind force as it exits.
  • Bent tubular trapezoids in most propellers have their entry surfaces smaller than their exit surfaces in order to increase the air pressure. With this technique the present invention will make the most of centrifugal and propelling forces coming from the engine. The same technique applies to wind generators but in this case bent trapezoids will have entry surfaces larger than exit surfaces in order to reduce air pressure, which multiplied by the large rotor surface will produce an important quantity of energy making the most of the wind force on the wind rotor.
  • Round honeycomb rotors for wind generators and most propellers will have many round bent tubular trapezoids with a surface that multiplies over twenty times in relation to conventional rotors. Their large wind contact surfaces multiply the force on the wind rotor by having all its outwards perimeters completely shut down.
  • Round honeycomb rotors for wind generators and most propellers with round bent tubular trapezoids have the advantage of multiplying the number of trapezoids and therefore also multiplying the wind contact surface or wind friction on bent pieces thus maximising wind force on the rotor, which in most cases will also be multiplied. Taking into account that trapezoid perimeters will be completely closed by concentric tubular cylinders being optional to have every row lined up or not. This is the foundation of the present patent.
  • Round honeycomb rotors for wind generators and most propellers will be capable of moving in both directions depending on how the bent pieces in between round bent tubular trapezoids are positioned.
  • FIG. 1 is a front view of the round honeycomb rotor for wind generators, in which we can appreciate several concentric tubular cylinders ( 1 ) (the drawing shows four tubular cylinders).
  • the tubular cylinder with largest diameter has a funnel fitted in ( 4 ) with a conical shape being open outwards in order to maximise the wind entry surface.
  • These tubular cylinders have bent tubular trapezoids ( 2 ) fitted in between each of them (the drawing shows twelve/ten/eight/six bent trapezoids in between each concentric cylinder starting with the one having largest diameter and alternating from one diameter to the other).
  • FIG. 2 is a front view of the round honeycomb rotor for most propellers, in which we can appreciate several concentric tubular cylinders ( 6 ) (the drawing shows four).
  • the tubular cylinder with largest diameter has a funnel fitted in ( 9 ) with a conical shape being open inwards in order to minimise the wind exit surface.
  • These concentric cylinders have bent pieces ( 7 ) fitted in between each of them (the drawing shows twelve/ten/eight/six bent pieces in between each concentric cylinder starting with the one having largest diameter and alternating from one diameter to the other). This explains the round honeycomb shape with round bent tubular trapezoids ( 10 ).
  • the cube or nucleus ( 8 ) which will have the alternator axis fitted in.
  • FIG. 3 shows a section of FIG. 1 where we can see a section of a concentric tubular cylinder ( 1 ) with the cube or nucleus in the middle ( 3 ) and trapezoids width proportions ( 2 ), in which we can appreciate their bending.
  • the tubular cylinder with largest diameter how a conical shaped funnel is fitted in ( 4 ) opening outwards.
  • Round bent tubular trapezoids ( 5 ) also have arrows indicating the wind direction.
  • FIG. 4 shows a section of FIG. 2 where we can see several concentric tubular cylinders ( 6 ) with the cube or nucleus in the middle ( 8 ) and trapezoids width proportions ( 7 ). We can also appreciate on the tubular cylinder with largest diameter how a conical shaped funnel is fitted in ( 4 ) opening inwards in order to minimise the wind exit surface. Round bent tubular trapezoids ( 10 ) also have arrows indicating the wind direction.
  • FIG. 5 shows half a section of the wind generator largest tubular cylinder, in which we can appreciate the bending of the pieces fitted in between each round bent tubular trapezoids. We can also appreciate the reduction of wind exit surface in wind generators according to the direction of the “V” arrow and the spin direction according to the “R” arrow.
  • FIG. 6 shows half a section of most propellers largest tubular cylinder, in which we can appreciate the bending of the pieces fitted in between each round bent tubular trapezoids. We can also appreciate the reduction of wind entry surface being the wind exit surface larger, the direction of the wind entrance according to the “C” arrow and the spin direction according to the “H” arrow.
  • Round honeycomb rotor for wind generators and most propellers with four or more round bent tubular trapezoids is composed of a nucleus ( 3 , 7 ), which is the centre or the rotor; two or more tubular cylinders ( 1 , 5 ) concentrically mounted with pieces ( 2 , 6 ) fitted in between them and forming the round bent tubular trapezoids.
  • the tubular cylinder with largest diameter ( 1 ) will have a conical shaped funnel ( 4 ) fitted in its entrance and opening outwards.
  • the tubular cylinder with largest diameter ( 5 ) will have a conical shaped funnel ( 8 ) fitted in its exit and opening inwards.
  • wind generator rotor can vary according to the needed capacity being the diameters similar to the dimensions of traditional wind generators. Building materials will have to be light, metallic and corrosion resistant. As for most propellers rotor cast iron or highly resistant and light materials alloy as well as sheathing plastic are recommended.
  • Round bent tubular trapezoids ( 2 ) in wind generators will be mounted in order to minimise the wind exit. This is achieved with larger wind entry surfaces and smaller exit surfaces. Due to the smaller wind exit surface the light pressure that takes place is very important for the large rotor surface, which follows the “V” direction according to FIG. 5 .
  • propeller pieces and round bent tubular trapezoids ( 7 ) will be smaller at entry surfaces and larger at exit surfaces following the “C” direction according to FIG. 6 .
  • the cube or nucleus ( 3 , 8 ) will be fitted on the alternator axis or on the engine according to its fixing characteristics.

Abstract

Round honeycomb rotor for wind generators and most propellers has bent tubular trapezoids, two or more concentric tubular cylinders and a variable number of round bent tubular trapezoids. Both cylinders and trapezoids form modular trapezoidal tubes, which have large wind contact surfaces. The concentric tubular cylinders of the round panel have bent pieces fitted in between them whose function is to minimise wind exit and multiply wind contact surfaces in wind generators. As for propeller rotors the number of round bent tubular trapezoids gets multiplied as well as its wind contact surfaces, which results in the optimum use of most centrifugal propelling forces thanks to the reduction of wind entrance and the amplification of wind exit.

Description

This application is a national-stage entry under 35 U.S.C. § 371 based on International Application Serial No. PCT/ES2003/000344, filed Jul. 9, 2003.
The purpose of this patent invention called round honeycomb rotor with bent tubular trapezoids is ideal for wind generators and most propellers. Its purpose is to improve wind generators and propellers performance, which is achieved by a total closure of all the perimeters through the concentric tubular cylinders where the bent pieces, which are mounted upon the tubular cylinders lean on. Everything is assembled in a round honeycomb shape formed by modules of round bent tubular trapezoids, which by receiving all of the wind force multiply over two the number of trapezoids, which at the same time multiply wind contact surfaces over twenty times. Wind generator rotors make the most of the wind force thanks to the multiplication of trapezoids as well as the multiplication of their contact surfaces with the wind. The same applies to most propeller rotors, the multiplication of the number of trapezoids added to the multiplication of their contact surfaces lead to the multiplication and optimum use of the driving centrifugal forces involved.
STATE OF THE ART TECHNIQUE
The technique used in wind generator rotors has varied applications and counts with different dimensions. It generally consists of a pitch with usually three blades fitted in; some models have directional blades easily adaptable to the wind direction. Currently, wind generators and most propellers have their outer perimeters widely open being most of the driving centrifugal forces wasted through the propellers. Conventional wind generators, which have three blades with minimum contact surface, usually achieve quite a low performance in wind speed.
DESCRIPTION OF THE INVENTION
Round honeycomb rotors with round bent tubular trapezoids are ideal for wind generators and most propellers. They consist of several concentric tubular cylinders with bent pieces fitted in between making round tubular trapezoids whose main purpose is to maximise the wind force performance. On the one hand this maximisation in wind generators and propellers is possible by substituting the conventional blades with bent tubular trapezoids, which have the capacity to multiply wind contact surfaces over twenty times. On top of that propellers also maximise most of the propelled centrifugal forces coming from the engine revolutions and going to the blades. On the other hand these trapezoids are fitted into concentric tubular cylinders therefore closing all the trapezoids perimeters giving the rotor a round honeycomb shape. In wind generators the tubular cylinder with largest diameter has fitted in an open funnel with a conical opening facing outwards in order to increase the wind entry surface to the rotor. Bent tubular trapezoids in conventional wind generators have a soft entrance, which goes diminishing towards the exit creating a small pressure. This is natural in this kind of wind rotors as they have wind entrance and exit areas orientated in the same direction. Nevertheless in this present patent invention, the progressive curving of the bent tubular trapezoids will divert the course of the wind to another direction, which will automatically reduce the wind force as it exits like it happens in wind turbines. Propellers in general will have similar characteristics to wind rotors adding the effect of centrifugal forces. With regular winds round bent tubular trapezoids exit areas will have to be fixed or calculated in advance in order to achieve an adequate pressure. With variable winds exit areas will be automatic. The above mentioned round tubular trapezoids are assembled in several concentric tubular cylinders, which have bent pieces inserted in between each one of them giving the whole structure the shape of a round honeycomb with round bent tubular trapezoids inside. Bent tubular trapezoids in wind generators and propellers could be of any of the well-known geometrical shapes such as round, tubular, oval or polygons with as many regular or irregular sides as needed. Inside the trapezoids similar shapes could be adopted or even other ones such as oblique trapezoids or any rough shapes whose only function would be to minimise the wind force. The tubular cylinder with larger diameter in most propellers rotor has fitted in a conical funnel opening inwards that reduces the wind exit surface therefore minimising the wind force as it exits.
Bent tubular trapezoids in most propellers have their entry surfaces smaller than their exit surfaces in order to increase the air pressure. With this technique the present invention will make the most of centrifugal and propelling forces coming from the engine. The same technique applies to wind generators but in this case bent trapezoids will have entry surfaces larger than exit surfaces in order to reduce air pressure, which multiplied by the large rotor surface will produce an important quantity of energy making the most of the wind force on the wind rotor.
Round honeycomb rotors for wind generators and most propellers will have many round bent tubular trapezoids with a surface that multiplies over twenty times in relation to conventional rotors. Their large wind contact surfaces multiply the force on the wind rotor by having all its outwards perimeters completely shut down.
Round honeycomb rotors for wind generators and most propellers with round bent tubular trapezoids have the advantage of multiplying the number of trapezoids and therefore also multiplying the wind contact surface or wind friction on bent pieces thus maximising wind force on the rotor, which in most cases will also be multiplied. Taking into account that trapezoid perimeters will be completely closed by concentric tubular cylinders being optional to have every row lined up or not. This is the foundation of the present patent.
Round honeycomb rotors for wind generators and most propellers will be capable of moving in both directions depending on how the bent pieces in between round bent tubular trapezoids are positioned.
DRAWINGS DESCRIPTION
FIG. 1 is a front view of the round honeycomb rotor for wind generators, in which we can appreciate several concentric tubular cylinders (1) (the drawing shows four tubular cylinders). The tubular cylinder with largest diameter has a funnel fitted in (4) with a conical shape being open outwards in order to maximise the wind entry surface. These tubular cylinders have bent tubular trapezoids (2) fitted in between each of them (the drawing shows twelve/ten/eight/six bent trapezoids in between each concentric cylinder starting with the one having largest diameter and alternating from one diameter to the other). This explains the round honeycomb shape individually composed of round bent tubular trapezoids (5). Finally, we see right in the middle the cube or nucleus (3), which will have the alternator axis fitted in.
FIG. 2 is a front view of the round honeycomb rotor for most propellers, in which we can appreciate several concentric tubular cylinders (6) (the drawing shows four). The tubular cylinder with largest diameter has a funnel fitted in (9) with a conical shape being open inwards in order to minimise the wind exit surface. These concentric cylinders have bent pieces (7) fitted in between each of them (the drawing shows twelve/ten/eight/six bent pieces in between each concentric cylinder starting with the one having largest diameter and alternating from one diameter to the other). This explains the round honeycomb shape with round bent tubular trapezoids (10). Finally, we see right in the middle the cube or nucleus (8), which will have the alternator axis fitted in.
FIG. 3 shows a section of FIG. 1 where we can see a section of a concentric tubular cylinder (1) with the cube or nucleus in the middle (3) and trapezoids width proportions (2), in which we can appreciate their bending. We can also appreciate on the tubular cylinder with largest diameter how a conical shaped funnel is fitted in (4) opening outwards. Round bent tubular trapezoids (5) also have arrows indicating the wind direction.
FIG. 4 shows a section of FIG. 2 where we can see several concentric tubular cylinders (6) with the cube or nucleus in the middle (8) and trapezoids width proportions (7). We can also appreciate on the tubular cylinder with largest diameter how a conical shaped funnel is fitted in (4) opening inwards in order to minimise the wind exit surface. Round bent tubular trapezoids (10) also have arrows indicating the wind direction.
FIG. 5 shows half a section of the wind generator largest tubular cylinder, in which we can appreciate the bending of the pieces fitted in between each round bent tubular trapezoids. We can also appreciate the reduction of wind exit surface in wind generators according to the direction of the “V” arrow and the spin direction according to the “R” arrow.
FIG. 6 shows half a section of most propellers largest tubular cylinder, in which we can appreciate the bending of the pieces fitted in between each round bent tubular trapezoids. We can also appreciate the reduction of wind entry surface being the wind exit surface larger, the direction of the wind entrance according to the “C” arrow and the spin direction according to the “H” arrow.
DESCRIPTION OF A PREFERENTIAL PERFORMANCE
Round honeycomb rotor for wind generators and most propellers with four or more round bent tubular trapezoids is composed of a nucleus (3,7), which is the centre or the rotor; two or more tubular cylinders (1,5) concentrically mounted with pieces (2,6) fitted in between them and forming the round bent tubular trapezoids. In rotors for wind generators the tubular cylinder with largest diameter (1) will have a conical shaped funnel (4) fitted in its entrance and opening outwards. In rotors for most propellers the tubular cylinder with largest diameter (5) will have a conical shaped funnel (8) fitted in its exit and opening inwards. All these different pieces can be assembled by joint traditional methods such as welding, riveting or screwing. The dimensions for wind generator rotor can vary according to the needed capacity being the diameters similar to the dimensions of traditional wind generators. Building materials will have to be light, metallic and corrosion resistant. As for most propellers rotor cast iron or highly resistant and light materials alloy as well as sheathing plastic are recommended.
Round bent tubular trapezoids (2) in wind generators will be mounted in order to minimise the wind exit. This is achieved with larger wind entry surfaces and smaller exit surfaces. Due to the smaller wind exit surface the light pressure that takes place is very important for the large rotor surface, which follows the “V” direction according to FIG. 5.
In round honeycomb rotors, propeller pieces and round bent tubular trapezoids (7) will be smaller at entry surfaces and larger at exit surfaces following the “C” direction according to FIG. 6.
The cube or nucleus (3,8) will be fitted on the alternator axis or on the engine according to its fixing characteristics.
Once the industrial object of this present Invention patent has been presented and described clear and extensively enough as to be exploited, I declare it new and of my own invention. Accidental details such as shape, size, materials and building procedures could be subject of alteration according to what has been described and represented in this report if it remains within the speciality resumed in the following claims.

Claims (1)

1. A round honeycomb rotor for propellers comprising, curved tubular trapezoids comprising a set of pieces surrounded by tubular cylinders, at the center of said cylinders is an axle operably linked to an alternator or engine, wherein the perimeters of said pieces have round curved tubular trapezoidal shapes being peripherally enclosed by said tubular cylinders which are concentric among themselves and assembled in modules, the positions of said pieces between said concentric tubular cylinders coincide or alternate forming curved trapezoidal shaped tubes that are linked among themselves, wherein the structure of said rotor has a round honeycomb shape with the axle assembled in the middle and operably linked to an alternator or engine, and wherein each tubular cylinder comprises four or more of said pieces and the cylinders are assembled in one or more pairs, wherein said round trapezoidal pieces are curved to allow a larger wind contact surface to maximize wind performance, wherein said curved tubular trapezoids can have any known regular or irregular geometrical shape, wherein said round curved tubular trapezoids have smaller wind entry surfaces and larger wind exit surfaces, and wherein the tubular cylinder comprising the largest diameter comprises an exit funnel comprising a tubular conical shape that reduces wind exit surfaces.
US10/535,984 2003-07-09 2003-07-09 Windmill rotor comprising multiple separate wind channels Expired - Fee Related US7244103B2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/ES2003/000344 WO2005005823A1 (en) 2003-07-09 2003-07-09 Windmill rotor comprising multiple separate wind channels

Publications (2)

Publication Number Publication Date
US20060182632A1 US20060182632A1 (en) 2006-08-17
US7244103B2 true US7244103B2 (en) 2007-07-17

Family

ID=34043156

Family Applications (1)

Application Number Title Priority Date Filing Date
US10/535,984 Expired - Fee Related US7244103B2 (en) 2003-07-09 2003-07-09 Windmill rotor comprising multiple separate wind channels

Country Status (16)

Country Link
US (1) US7244103B2 (en)
EP (1) EP1548277B9 (en)
JP (1) JP4461282B2 (en)
CN (1) CN100419256C (en)
AT (1) ATE329153T1 (en)
AU (1) AU2003304328A1 (en)
BR (1) BR0314169A (en)
CA (1) CA2499514A1 (en)
DE (1) DE60305951T2 (en)
DK (1) DK1548277T3 (en)
EG (1) EG23578A (en)
ES (1) ES2263006T3 (en)
MX (1) MXPA05002174A (en)
MY (1) MY138382A (en)
PT (1) PT1548277E (en)
WO (1) WO2005005823A1 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100135809A1 (en) * 2007-04-05 2010-06-03 Hermann Olschnegger Wind wheel
US20120257971A1 (en) * 2011-04-11 2012-10-11 Scott Schmutzer WindJet ® Turbine Ring
US20120319403A1 (en) * 2011-05-20 2012-12-20 Fosdick George A Wheel Turbine Rotor
US20170138338A1 (en) * 2015-10-16 2017-05-18 Augustine Chan Turbinator

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008157174A1 (en) * 2007-06-13 2008-12-24 Skyron Systems, Inc. Wind turbine blade
CN103375343A (en) * 2012-04-17 2013-10-30 罗才德 Spiral pipe type wind power generator
USD761948S1 (en) * 2013-11-18 2016-07-19 Ebm-Papst Mulfingen Gmbh & Co. Kg Fan
WO2017065782A1 (en) * 2015-10-16 2017-04-20 Augustine Chan Turbinator
RS20180564A1 (en) * 2018-05-15 2019-11-29 Samardzija Nikola Air movement power multiplier

Citations (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US984599A (en) 1906-02-24 1911-02-21 Stephane Pichault Apparatus for storing and distributing wind-power.
US1232795A (en) * 1913-05-05 1917-07-10 Green Fuel Economizer Company Circular-disk fan.
US1263473A (en) * 1917-09-25 1918-04-23 Gen Electric Elastic-fluid turbine.
GB213022A (en) 1923-01-03 1924-03-27 Charles Esmond Nightingale Improvements in windmills and windmotors
US2503072A (en) * 1945-11-15 1950-04-04 Gen Electric Axial flow impeller
US3198423A (en) 1964-07-06 1965-08-03 Francis H Clute Helicoid fan
US3266734A (en) 1964-02-03 1966-08-16 Rolls Royce Thrust reversers for jet propulsion engines
US3485252A (en) 1966-04-26 1969-12-23 Rolls Royce Air intake duct for a gas turbine engine
US3783814A (en) 1968-01-23 1974-01-08 C Zovko Thrust augmenting expansion engine
US4080100A (en) 1976-09-28 1978-03-21 Mcneese Walter C Wind motor
DE2909781A1 (en) 1979-03-13 1980-09-25 Karlheinz Ohlberg Wind driven power generating turbine - has independent concentric rotors driving common generator to give higher efficiency
DE2951635A1 (en) * 1979-12-21 1981-07-02 Karlheinz Ing.(grad.) 4220 Dinslaken Ohlberg Wind power unit with vertical rotor shaft - uses counterweight of pendulum system to move rotor automatically out of wind when its force exceeds threshold
US4289450A (en) 1978-12-05 1981-09-15 Alberto Kling Rotor for operation in a flow medium
JPS5891376A (en) 1981-11-25 1983-05-31 Masao Yasugata Wind turbine
US5711653A (en) 1994-07-31 1998-01-27 Mccabe; Francis J. Air lifted airfoil
US5755557A (en) * 1995-08-03 1998-05-26 Valeo Thermique Moteur Axial flow fan
EP0953774A1 (en) 1998-04-01 1999-11-03 Eaton Corporation Fan assembly having increased fan blade area
US6599085B2 (en) 2001-08-31 2003-07-29 Siemens Automotive, Inc. Low tone axial fan structure
WO2004002821A1 (en) 2002-06-28 2004-01-08 Vtol Technologies Limited Ducted air power plant
WO2005085648A1 (en) 2004-02-25 2005-09-15 Sanchez Sanchez Felix Round honeycomb rotor
WO2006045856A1 (en) 2004-10-29 2006-05-04 Sanchez Sanchez Felix Air-jet propeller

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2382381A (en) * 2001-11-21 2003-05-28 John Freer Green Improvements in wind turbines

Patent Citations (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US984599A (en) 1906-02-24 1911-02-21 Stephane Pichault Apparatus for storing and distributing wind-power.
US1232795A (en) * 1913-05-05 1917-07-10 Green Fuel Economizer Company Circular-disk fan.
US1263473A (en) * 1917-09-25 1918-04-23 Gen Electric Elastic-fluid turbine.
GB213022A (en) 1923-01-03 1924-03-27 Charles Esmond Nightingale Improvements in windmills and windmotors
US2503072A (en) * 1945-11-15 1950-04-04 Gen Electric Axial flow impeller
US3266734A (en) 1964-02-03 1966-08-16 Rolls Royce Thrust reversers for jet propulsion engines
US3198423A (en) 1964-07-06 1965-08-03 Francis H Clute Helicoid fan
US3485252A (en) 1966-04-26 1969-12-23 Rolls Royce Air intake duct for a gas turbine engine
US3783814A (en) 1968-01-23 1974-01-08 C Zovko Thrust augmenting expansion engine
US4080100A (en) 1976-09-28 1978-03-21 Mcneese Walter C Wind motor
US4289450A (en) 1978-12-05 1981-09-15 Alberto Kling Rotor for operation in a flow medium
DE2909781A1 (en) 1979-03-13 1980-09-25 Karlheinz Ohlberg Wind driven power generating turbine - has independent concentric rotors driving common generator to give higher efficiency
DE2951635A1 (en) * 1979-12-21 1981-07-02 Karlheinz Ing.(grad.) 4220 Dinslaken Ohlberg Wind power unit with vertical rotor shaft - uses counterweight of pendulum system to move rotor automatically out of wind when its force exceeds threshold
JPS5891376A (en) 1981-11-25 1983-05-31 Masao Yasugata Wind turbine
US5711653A (en) 1994-07-31 1998-01-27 Mccabe; Francis J. Air lifted airfoil
US5755557A (en) * 1995-08-03 1998-05-26 Valeo Thermique Moteur Axial flow fan
EP0953774A1 (en) 1998-04-01 1999-11-03 Eaton Corporation Fan assembly having increased fan blade area
US6599085B2 (en) 2001-08-31 2003-07-29 Siemens Automotive, Inc. Low tone axial fan structure
WO2004002821A1 (en) 2002-06-28 2004-01-08 Vtol Technologies Limited Ducted air power plant
WO2005085648A1 (en) 2004-02-25 2005-09-15 Sanchez Sanchez Felix Round honeycomb rotor
WO2006045856A1 (en) 2004-10-29 2006-05-04 Sanchez Sanchez Felix Air-jet propeller

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
International Search Report for PCT/ES2003/000344 dated Oct. 23, 2003.
Translation of the International Preliminary Examination Search Report for PCT/ES2003/000344 dated Jul. 12, 2005.

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100135809A1 (en) * 2007-04-05 2010-06-03 Hermann Olschnegger Wind wheel
US20120257971A1 (en) * 2011-04-11 2012-10-11 Scott Schmutzer WindJet ® Turbine Ring
US20120319403A1 (en) * 2011-05-20 2012-12-20 Fosdick George A Wheel Turbine Rotor
US20170138338A1 (en) * 2015-10-16 2017-05-18 Augustine Chan Turbinator

Also Published As

Publication number Publication date
MY138382A (en) 2009-05-29
ATE329153T1 (en) 2006-06-15
BR0314169A (en) 2005-07-19
JP2006526100A (en) 2006-11-16
PT1548277E (en) 2006-09-29
DE60305951T2 (en) 2007-01-25
EP1548277A1 (en) 2005-06-29
EG23578A (en) 2006-08-17
EP1548277B9 (en) 2006-10-11
CN1695007A (en) 2005-11-09
EP1548277B1 (en) 2006-06-07
CA2499514A1 (en) 2005-01-20
ES2263006T3 (en) 2006-12-01
MXPA05002174A (en) 2005-05-23
CN100419256C (en) 2008-09-17
WO2005005823A1 (en) 2005-01-20
US20060182632A1 (en) 2006-08-17
AU2003304328A1 (en) 2005-01-28
JP4461282B2 (en) 2010-05-12
DK1548277T3 (en) 2006-10-09
DE60305951D1 (en) 2006-07-20

Similar Documents

Publication Publication Date Title
US20070077145A1 (en) Omni directional baffled wind energy power converter apparatus and method
US7244103B2 (en) Windmill rotor comprising multiple separate wind channels
US5969430A (en) Dual turbine wind/electricity converter
US6041596A (en) Building structure for utilization of wind power
US4368007A (en) Fluid driven turbine
CA2769655A1 (en) Omnidirectional vertical-axis wind turbine
US9013054B1 (en) Wind turbine with channels and roof air exhaust
WO2007111532A1 (en) Shpadi propeller (variants) and the involute of the blades thereof
WO2008045237A2 (en) Wind power converting apparatus and method
US4890976A (en) Wind turbine
US10648450B2 (en) Wind turbine suitable for mounting without a wind turbine tower
JP6954739B2 (en) Rotor for generator
AU2010264534B2 (en) Wind turbine
KR20080052820A (en) Aerogenerator
KR20060103085A (en) Round honeycomb rotor
US20100098543A1 (en) Rotor structure of wind turbine
UA19718U (en) Round cellular rotor
US20110309633A1 (en) Wind Auger
KR101764152B1 (en) Turbine type power generator with vertical axis
CZ2005142A3 (en) Windmill rotor comprising multiple separate wind channels
US11300095B2 (en) Wind turbine suitable for mounting without a wind turbine tower
KR102470537B1 (en) variable blade aberration
EA007439B1 (en) Vortical unit
CA1280697C (en) Wind turbine
KR20130017770A (en) The case of wind blades considering the difference of internal wind speeds-induced internal pressure drop and the complex vertical-axis wind blades which are built into this case

Legal Events

Date Code Title Description
REMI Maintenance fee reminder mailed
LAPS Lapse for failure to pay maintenance fees
STCH Information on status: patent discontinuation

Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362

FP Lapsed due to failure to pay maintenance fee

Effective date: 20110717